发明名称 Shock absorber for a jet propulsion system.
摘要 <p>A system with a flow of compressible fluid which is very rapidly pressurised, comprising a fluid outflow channel (8 + 9) characterised in that it comprises, inside this channel a shock wave damper (30, 30') having at least one rigid disc (33, 34) transverse to this channel, of maximum cross-section less than the local cross-section (9A) of this channel. &lt;IMAGE&gt;</p>
申请公布号 EP0508851(A1) 申请公布日期 1992.10.14
申请号 EP19920400811 申请日期 1992.03.25
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 GARNERO, PASCAL;SIEGWALD, ROLAND
分类号 F02K9/97;F02K9/38 主分类号 F02K9/97
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